A method of assembling a planetary gearset includes die-forming a plurality of circumferentially spaced apart teeth on a sun gear, a planet gear and a ring gear. Each tooth includes a pair of tooth flanks in a final net form for engagement with mating gear teeth. The sun gear teeth have a conical shape to allow a first die to linearly move relative to a second die after the gear teeth are die-formed. The planet gears are mounted on a carrier. The sun gear and the planet gear are oriented such that the conical shapes of the respective gear teeth taper in opposite directions from one another and the planet gear teeth meshingly engage with both the ring gear teeth and the sun gear teeth.
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1. A method of assembling a planetary gearset, comprising:
die-forming a plurality of circumferentially spaced apart teeth on a sun gear, each tooth having a pair of tooth flanks in a final net form for engagement with mating gear teeth, the sun gear teeth having a conical shape to allow a first die to linearly move relative to a second die after the sun gear teeth are die-formed;
die-forming a plurality of circumferentially spaced apart teeth on a planet gear, each planet gear tooth having a pair of tooth flanks shaped in a final net form for engagement with mating sun gear tooth flanks, the planet gear teeth having a conical shape to allow a first die to linearly move relative to a second die after the planet gear teeth are die-formed;
die-forming a plurality of circumferentially spaced apart teeth on a ring gear, each ring gear tooth having a pair of tooth flanks shaped in a final net form for engagement with mating planet gear tooth flanks, the ring gear teeth having a conical shape to allow a first die to linearly move relative to a second die after the ring gear teeth are die-formed;
rotatably mounting the planet gear on a carrier;
orienting the sun gear and the planet gear such that the conical shapes of the respective gear teeth taper in opposite directions from one another; and
meshingly engaging the planet gear teeth with both the ring gear teeth and the sun gear teeth.
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This application is a 371 U.S. National Stage of International Application No. PCT/US2011/060146, filed Nov. 10, 2011, and claims priority to U.S. Provisional application No. 61/427,824, filed Dec. 29, 2010, the disclosures of which are herein incorporated by reference in their entirety.
The present disclosure relates to a planetary gear drive for a power transmission mechanism. More particularly, the gears of the planetary gear drive each include a beveloid shape such that the gears may be manufactured using a die forming process.
This section provides background information related to the present disclosure which is not necessarily prior art.
Planetary gearsets have been widely used in various power transmission devices to provide a torque multiplying or gear reduction function. Planetary gearsets typically include a sun gear, a ring gear and one or more planet gears continuously meshed with the sun and ring gears. The shape of each of these gears is typically based on a cylinder having circumferentially spaced apart teeth formed on an external or internal surface of the cylinder. The gear teeth may have a spur or helical shape.
Known processes used to manufacture the gears of a planetary gearset include hobbing, shaping, rolling, shaving, grinding and planing. Some gears, such as a ring gear having spur teeth, may be formed using a broaching process. Each of the previously described known processes require very expensive machines to form an involute shape on the gear tooth flanks. These processes are relatively time consuming and expensive. Accordingly, it may be beneficial to develop a different gear forming process to reduce the time and cost required to form the gear teeth.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
A method of assembling a planetary gearset includes die-forming a plurality of circumferentially spaced apart teeth on a sun gear, a planet gear and a ring gear. Each tooth includes a pair of tooth flanks in a final net form for engagement with mating gear teeth. The sun gear teeth have a conical shape to allow a first die to linearly move relative to a second die after the gear teeth are die-formed. The planet gears are mounted on a carrier. The sun gear and the planet gear are oriented such that the conical shapes of the respective gear teeth taper in opposite directions from one another and the planet gear teeth meshingly engage with both the ring gear teeth and the sun gear teeth.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
An axially moveable sleeve 22 is splined to output shaft 18 to be axially moveable between three drive positions. In the position depicted in
Sleeve 22 may be axially moved to the left as viewed in
In a low range mode of operation, sleeve 22 is further axially displaced to the left to drivingly engage spline 24 with an internal spline 28 formed on a carrier 30 of planetary gearset 20. In the low range mode of operation, output shaft 18 rotates at a reduced speed relative to input shaft 14.
Planetary gearset 20 includes a sun gear 32 integrally formed with input shaft 14. A ring gear 34 is restricted from rotation relative to housing 12. A plurality of planet gears 36 are circumferentially spaced apart from one another and each planet gear 36 is in constant meshed engagement with sun gear 32 and ring gear 34. Each planet gear 36 is rotatably supported on a pin 40 fixed to carrier 30. Carrier 30 includes a front plate 42 and a rear plate 44 fixed to one another. A plurality of bushings or bearings 48 rotatably support each planet gear 36 on one of respective pins 40. Washers 50, 52 axially position planet gears 36 between front plate 42 and rear plate 44.
Sun gear 32 includes a plurality of circumferentially spaced apart teeth 60. Each tooth 60 includes a pair of tooth flanks 62 having an involute shape. Each tooth 60 is conically shaped such that a first end 66 of tooth 60 includes a crest 68 defining a smaller outer diameter than crest 68 defines at an opposite end 70 of tooth 60. The tooth design defines an involute tooth form that is tapered in an axial perspective while maintaining symmetry about a standard cylindrical generating base diameter. By shaping sun gear 32 in this manner, integral input shaft and sun gear 32 may be constructed using a die forming process.
For example, and in reference to
Subsequent machining processes to other portions of input shaft 14 may be performed but tooth flank surfaces 62 remain untouched after die forming. Depending on the size and geometry of the sun gear being formed, the die forming process may be completed within a single die stroke within a single cavity, or a multiple cavity progressive forming process may be utilized. A progressive densification through multiple die strikes may be used to form a hardened layer at the exterior surfaces of sun gear 32. The mechanical properties of the hardened layer are similar to those defined using a case hardening process.
Each of planet gears 36 includes a plurality of circumferentially spaced apart teeth 80 also defined by a die forming process. Each of teeth 80 includes a pair of tooth flanks 84 having a beveloid or conical shape about an axis of rotation 88 as well as an involute form for the gear meshing surface. Planet gears 36 are constructed using a similar die forming process as described in relation to sun gear 32. The gear tooth beveloid or cone angle for the planet gears is the same as the conical angle used to define sun gear 32. Because planet gears 36 rotate along an axis parallel to and spaced apart from axis of rotation 74, planet gears 36 are positioned such that the conical surfaces of gear teeth 80 complement gear teeth 60 of sun gear 32. Stated another way, the cones of the interconnecting gears open in opposite directions.
Ring gear 34 includes a plurality of spaced apart teeth 92 having a beveloid shape to allow driving meshed interconnection between teeth 80 of planet gears 36 and teeth 92 of ring gear 34. Ring gear 34 is contemplated as being constructed using the die forming process previously described in relation to sun gear 32. As such, each of gear teeth 60, 80 and 92 are net formed including two flanks that do not require further material displacement after the die forming process has been completed.
Use of the parallel axis conical gear design previously described provides an additional advantage of adjusting the back lash of the gearset during the gear assembly process. A back lash adjustment may be accomplished by shimming the axial position of each gear which increases or decreases the clearance between the gear teeth due to the axially tapered tooth form. Washers 50, 52 may be constructed having different thicknesses functioning as shims changing the axial position of planet gears 36 relative to sun gear 32 and ring gear 34.
The foregoing description of the embodiments has bee provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
Wenthen, David W., Smith, Burke, Fitzgerald, Brian
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Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
May 31 2011 | WENTHEN, DAVID W | MAGNA POWERTRAIN OF AMERICA, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 028194 | /0479 | |
May 31 2011 | SMITH, BURKE | MAGNA POWERTRAIN OF AMERICA, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 028194 | /0479 | |
Sep 30 2011 | FITZGERALD, BRIAN M | MAGNA POWERTRAIN OF AMERICA, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 028194 | /0479 | |
Nov 10 2011 | Magna Powertrain of America, Inc. | (assignment on the face of the patent) | / |
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